Process of calculation with regard to probable size and first stage thrust for Sputnik launching vehicle is attempted, assuming vehicle to be "standard" 3-stage tandem rocket; assumptions regarding fuel and oxidizer used; trajectory is approximated by trolley car equations; table shows comparison of Vanguard and Sputnik; payload optimization for Sputnik III. (See also SAE -- Paper n S154 for meeting Dec 17 1958 (No. Calif Sec) 10 p)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparison of Vanguard and Sputnik launching vehicles


    Weitere Titelangaben:

    SAE -- J


    Beteiligte:
    Kramer, S.B. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    COMPARISON OF VANGUARD AND SPUTNIK LAUNCHING VEHICLES

    KRAMER, SAUNDERS B. | SAE Technical Papers | 1958


    Comparison of Vanguard and Sputnik launching vehicles

    Kramer, S.B. | Engineering Index Backfile | 1958


    Sputnik and Vanguard: comparison

    Koelle, H.H. | Engineering Index Backfile | 1957


    Sequence diagram analysis of vanguard satellite launching vehicle

    Escher, W.J.D. / Foster, R.W. | Engineering Index Backfile | 1961